View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 55827U 26145.37637137 +.00000000 +00000-0 +21109-3 0 00001
2 55827 87.9181 278.9773 0001860 93.5343 266.6003 13.20769795 00
| Epoch (UTC): | 25 May 2026 09:01:58 |
| Eccentricity: | 0.0001860 |
| inclination: | 87.9181° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9773° |
| argument of perigee: | 93.5343° |
| revolutions per day: | 13.20769795 |
| mean anomaly at epoch: | 266.6003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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